Dynamics of Flexible Space Vehicles with Active Attitude Control

Physics

Scientific paper

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Scientific paper

The implications of flexible appendages on the attitude dynamics of a space vehicle are examined in general terms. Two families of natural vibration modes, referred to as ‘constrained’ and ‘unconstrained’, are discussed and the relationships between them derived. The incorporation of either set of modes into a simulation of the general attitude motion (under the influence of perturbing torques and control torques) is explained. The influence of rotors on these results is also explored.

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